Home CFD Group

Indian Institute of Technology. Much of the computational work is done on a Linux-based high-performance compute cluster set up in our lab. In-house parallel CFD codes are routinely used for three-dimensional simulation of practical geometries like hypersonic inlets for scramjet engines and reentry capsules. Majority of the research is funded by Indian defense and space programmes. Paper titled Variable turbulent Prandtl number model for shockboundary-layer interaction authored by Subhajit Roy, Utkars.

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The website hypersonic-cfd.com currently has a traffic classification of zero (the smaller the more users). We have examined seven pages within the site hypersonic-cfd.com and found one website referring to hypersonic-cfd.com. We were able to detect one contacts and directions for hypersonic-cfd.com to help you correspond with them. We were able to detect one mass networking sites owned by hypersonic-cfd.com. The website hypersonic-cfd.com has been on the internet for six hundred and twenty-three weeks, nine days, three hours, and fifty minutes.
Pages Crawled
7
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1
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1
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1
Online Since
Oct 2012

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HYPERSONIC-CFD.COM HISTORY

The website hypersonic-cfd.com was registered on October 26, 2012. This web page was changed on the date of October 22, 2013. This domain will go back on the market on the date of October 26, 2014. It is now six hundred and twenty-three weeks, nine days, three hours, and fifty minutes young.
REGISTERED
October
2012
UPDATED
October
2013
EXPIRED
October
2014

COMPANY SPAN

11
YEARS
11
MONTHS
8
DAYS

LINKS TO DOMAIN

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HYPERSONIC-CFD.COM SERVER

I discovered that the main root page on hypersonic-cfd.com took two hundred and fifty-three milliseconds to stream. We could not observe a SSL certificate, so our parsers consider this site not secure.
Load time
0.253 secs
SSL
NOT SECURE
Internet Protocol
192.232.223.76

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Home CFD Group

DESCRIPTION

Indian Institute of Technology. Much of the computational work is done on a Linux-based high-performance compute cluster set up in our lab. In-house parallel CFD codes are routinely used for three-dimensional simulation of practical geometries like hypersonic inlets for scramjet engines and reentry capsules. Majority of the research is funded by Indian defense and space programmes. Paper titled Variable turbulent Prandtl number model for shockboundary-layer interaction authored by Subhajit Roy, Utkars.

PARSED CONTENT

The website hypersonic-cfd.com had the following in the site, "Much of the computational work is done on a Linux-based high-performance compute cluster set up in our lab." We analyzed that the website stated " In-house parallel CFD codes are routinely used for three-dimensional simulation of practical geometries like hypersonic inlets for scramjet engines and reentry capsules." It also stated " Majority of the research is funded by Indian defense and space programmes. Paper titled Variable turbulent Prandtl number model for shockboundary-layer interaction authored by Subhajit Roy, Utkars."

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